Thermal protection system for the Galileo mission atmospheric entry probe
Author:
Affiliation:
1. General Electric Co., Philadelphia, Pa.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1980-358
Reference21 articles.
1. Development of a steady-state shape change ablation code for the design of outer planet probes
2. An approximate inviscid radiating flow field analysis for outer planet entry probes
3. Aerothermal environment for Jovian entry probes
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